View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 18422U 87088B 24260.83755682 .00001720 00000-0 20148-3 0 9994
2 18422 82.5119 213.7566 0018844 356.8029 3.3063 14.84380666973340
| Epoch (UTC): | 16 September 2024 20:06:04 |
| Eccentricity: | 0.0018844 |
| inclination: | 82.5119° |
| perigee height: | 602 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 213.7566° |
| argument of perigee: | 356.8029° |
| revolutions per day: | 14.84380666 |
| mean anomaly at epoch: | 3.3063° |
| orbit number at epoch: | 97334 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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